# Service difficulty reports: N825AX, cancelled Apr 25, 2007

A list on [N825AX, cancelled Apr 25, 2007](https://openairdocs.org/deregistered/N825AX-2007-04-25.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 155 reports

- [SDR ABXA060079](https://openairdocs.org/sdr/ABXA060079.md): Landing Gear · malfunctioned · Feb 2, 2006 · N825AX · Doug DC863 · Landing Gear System
  > AFTER TAKEOFF AT ILN, UNABLE TO RAISE LANDING GEAR HANDLE. DID NOT USE FLIGHT HANDLE RELEASE, AIRCRAFT WAS IN FLIGHT MODE. CREW FLEW AIRCRAFT WITH ALL THREE GEAR DOWN, DID A FLY BY TO VERIFY NOSE GEAR WAS STRAIGHT DOWN. COMPLIED WITH NOSE LANDING GEAR REPAC
- [SDR ABXA060041](https://openairdocs.org/sdr/ABXA060041.md): Stringer · cracked · Jan 15, 2006 · N825AX · Doug DC863 · Wing, Longeron/Stringer
  > LEFT WING (AFT SIDE) STRINGER LONGERON 58 WS 428 - 463 END FITTING CRACKED. REMOVED DAMAGED STRINGER END FITTING TWO CRACKS, ONE 4.5" AND ONE 12.0". FABRICATED NEW FITTING IAW DAC DWG 5644972. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2. PERFORMED D
- [SDR ABXA060045](https://openairdocs.org/sdr/ABXA060045.md): Spar Cap · corroded · Jan 14, 2006 · N825AX · Doug DC863 · Fuselage Main, Plate/Skin
  > WING CENTER SECTION UPPER SURFACE HAD TWO AREAS OF CORROSION WITH PITTING BS 851, RIGHT BUTT LINE 12, BS 851, RIGHT BUTT LINE 17. CUT OUT DAMAGED AREA AND REPAIRED WITH NEW PART IAW DC8 SRM 53-2-5. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 S
- [SDR ABXA060043](https://openairdocs.org/sdr/ABXA060043.md): Fitting · corroded · Jan 14, 2006 · N825AX · Doug DC863 · Fuselage Main, Attach Fittings
  > BATHTUB FITTING HAD CORROSION AT LONGERON 34, ATTACH POINT BS 879. CORROSION FOUND OUT OF LIMITS OF DC8 SRM 53-2-0. REMOVED FITTING IAW DC8 SRM 51-1-20D. INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-20D, 51-3-1, AND 51-1-8.
- [SDR ABXA060044](https://openairdocs.org/sdr/ABXA060044.md): Fitting · corroded · Jan 13, 2006 · N825AX · Doug DC863 · Fuselage Main, Attach Fittings
  > BATHTUB FITTING HAD CORROSION AT LONGERON 24, ATTACH POINT BS 940. CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-20. INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-20D, 51-3-0, AND 51-1-8.
- [SDR ABXA060042](https://openairdocs.org/sdr/ABXA060042.md): Skin · corroded · Jan 12, 2006 · N825AX · Doug DC863 · Fuselage Main, Plate/Skin
  > DEFOLIATED SKIN ON BELLY OF PLANE JUST AFT OF SKIN DOUBLER AT APPROXIMATELY STA 1420, LONGERON 36. REPAIRED AREA IAW ABX REA D853-51398-MR.
- [SDR ABXA060046](https://openairdocs.org/sdr/ABXA060046.md): Strap · corroded · Dec 23, 2005 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE STRAP ON TOP OF MAIN LANDING GEAR WHEEL WELL BOX FORWARD OF FLOORBEAM STA 902, LEFT BUTT LINE 65. REMOVED CORROSION IAW DC8 SRM 51-1-8. DETERMINED TO BE OUT OF ACCEPTABLE LIMITS IAW DC8 SRM 53-2-0. REMOVED AND REPLACED WITH NEW FABRICATED
- [SDR ABXA050263](https://openairdocs.org/sdr/ABXA050263.md): Cabin Pressure · unknown · Nov 4, 2005 · N825AX · Doug DC863 · Cabin Pressure Control System
  > DURING CLIMB AT FL310, CABIN RATE OF CLIMB WENT FROM 500 FPM TO 6,000 FPM. COULD NOT STOP THE CABIN FROM CLIMBING USING AUTO OR MANUAL LEVER. CABIN WENT TO 11,000 FT. DONNED OXYGEN AND STARTED DESCENT. AT ABOUT FL290, REGAINED CONTROL OF BOTH AUTO AND MANU
- [SDR ABXA050179](https://openairdocs.org/sdr/ABXA050179.md): Transmitter · defective · Jul 28, 2005 · N825AX · Doug DC863 · Engine Oil Pressure
  > NR 3 ENGINE OIL PRESSURE PEGGED OFF SCALE HIGH. ENGINE WAS SECURED AND FLIGHT CONTINUED ON TO IAD. OIL PRESSURE REMAINED PEGGED OUT HIGH. PERFORMED ENGINE INSPECTION IAW P&W JT3D MM 72-00. OIL FILTER FOUND CLEAN. REMOVED AND REPLACED OIL PRESSURE TRANSMIT
- [SDR ABXA040351](https://openairdocs.org/sdr/ABXA040351.md): Outflow Valve · malfunctioned · Oct 15, 2004 · N825AX · Doug DC863 · Pressure Regulator/Outflow Valve
  > DURING DESCENT, CABIN PRESS WENT TO 2000 FT/MIN. RATE OF CLIMB UP TO 9500 CABIN ALT WITH NO CONTROL EITHER MANUALLY OR AUTOMATICALLY. RECOVERED AT FL 19000. COULD NOT DUPLICATE. CREW VERBAL, HEAVY RAINS LEAVING ILN. SUSPECT ICE BUILD-UP. INSPECTED OUTFLO
- [SDR ABXA040155](https://openairdocs.org/sdr/ABXA040155.md): Control Box · defective · Apr 27, 2004 · N825AX · Doug DC863 · Landing Gear Position and Warning
  > AFTER TAKEOFF, GEAR WARNING LIGHT REMAINED ON. LANDING GEAR AND DOOR INDICATOR PANEL SHOWED NOSE GEAR. RECYCLED, SAME RESULT. CONSULTED ABNORMAL AND PROCEEDED TO DESTINATION. MAINTENANCE AT ILN: DURING SELF TEST OF PROX SWITCH CONTROL BOX, NOSE GEAR UP LIMIT F
- [SDR ABXA040058](https://openairdocs.org/sdr/ABXA040058.md): Angle · gouged · Jan 30, 2004 · N825AX · Doug DC863 · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP STA 219 FOLD HINGE COVER WELL OUTBOARD LOWER SIDE GOUGED. REPAIRED AREA IAW REA D827-48510MR.
- [SDR ABXA040054](https://openairdocs.org/sdr/ABXA040054.md): Longeron · corroded · Jan 30, 2004 · N825AX · Doug DC863 · Fuselage Main, Longeron/Stringer
  > FORWARD ACCESSORY AT STA 25, LONGERON 31 LEFT WAS CORRODED. REPAIRED AREA IAW REA D853-48515MR.
- [SDR ABXA040057](https://openairdocs.org/sdr/ABXA040057.md): Spar · cracked · Jan 30, 2004 · N825AX · Doug DC863 · Wing Spar
  > RIGHT WING REAR SPAR XRS 139 JACKPAD TO REAR SPAR FITTING CRACKED. REPAIRED AREA IAW REA D857-48845MR.
- [SDR ABXA040056](https://openairdocs.org/sdr/ABXA040056.md): Finger Doubler · corroded · Jan 30, 2004 · N825AX · Doug DC863 · Fuselage Main, Plate/Skin
  > FORWARD CARGO LOWER LEFT SKIN FINGER DOUBLER CORRODED UNDERNEATH FROM STA 200 TO 220, LONGERON 35 LEFT TO 33 LEFT, BUTTLINE 7 TO BUTTLINE 20. REPAIRED AREA IAW REA D853-48505MR.
- [SDR ABXA040053](https://openairdocs.org/sdr/ABXA040053.md): Longeron · cracked · Jan 30, 2004 · N825AX · Doug DC863 · Fuselage Main, Longeron/Stringer
  > RIGHT WHEEL WELL LONGERON 24 FITTING WAS CRACKED JUST UNDER BOTTLE BOLT. REMOVED AND REPLACED LONGERON 24 RIGHT IAW ABX REA D853-48504MR.
- [SDR ABXA040055](https://openairdocs.org/sdr/ABXA040055.md): Longeron · corroded · Jan 30, 2004 · N825AX · Doug DC863 · Fuselage Main, Longeron/Stringer
  > AFT ACCESSORY COMPARTMENT CORROSION AT FUSELAGE SKIN AND DOUBLER LONGERON 33 RIGHT, FS 1620 - 1628, ADJACENT TO OUTFLOW VALVE. REPAIRED AREA IAW REA D853-48508MR.
- [SDR ABXA030435](https://openairdocs.org/sdr/ABXA030435.md): Battery Pack · discharged · Nov 7, 2003 · N825AX · Doug DC863 · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHT BATTERY DEAD. REPLACED EMERGENCY BATTERY PACK. SYSTEM CHECKED GOOD IAW DC8 MM 33.
- [SDR ABXA030394](https://openairdocs.org/sdr/ABXA030394.md): Transmitter · defective · Oct 23, 2003 · N825AX · Doug DC863 · Engine Oil Pressure
  > NR 4 ENGINE OIL PRESSURE INDICATED + 100 PSI AT TOP OF CLIMB. SECURED ENGINE AT 0325Z, RETURNED TO 22 PSI AT 0345. REPLACED NR 4 OIL PRESSURE TRANSMITTER, NR 4 OIL PRESSURE RELIEF VALVE AND MAIN ENGINE OIL FILTER. RAN NR 4 ENGINE, OIL PRESSURE AT IDLE 41 PS
- [SDR ABXA030096](https://openairdocs.org/sdr/ABXA030096.md): Longeron · corroded · Mar 3, 2003 · N825AX · Doug DC863 · Fuselage Main, Longeron/Stringer
  > DURING LINE OPERATIONS AT ILN, LONGERON 36 WAS FOUND TO HAVE INTERGRANULAR CORROSION IN THE LOWER FLANGE AT STA 1420. REPAIRED LONGERON IAW ABX REA D853-46872MR.
- [SDR ABXA030066](https://openairdocs.org/sdr/ABXA030066.md): Threshold · bent · Feb 6, 2003 · N825AX · Doug DC863 · Fuselage Main, Structure
  > MAIN CABIN DOOR THRESHOLD LIP WAS RAISED PREVENTING DOOR FROM OPENING. REPAIRED RAISED LIP ON THRESHOLD OF MAIN CABIN DOOR AS REQUIRED IAW DC-8 MM.
- [SDR ABXA020347](https://openairdocs.org/sdr/ABXA020347.md): Control Arm · defective · Dec 6, 2002 · N825AX · Doug DC863 · Landing Gear Position and Warning
  > WITH GEAR HANDLE DOWN, GREEN LIGHTS NOT ON, RED LIGHTS NOT ON EITHER. ACCOMPLISHED ABNORMAL PROCEDURE, STILL NO LIGHTS. OTHER CHECKLIST ITEMS INDICATED ALL GEAR WAS DOWN AND LOCKED. FOUND GEAR WARNING INTERLOCK CIRCUIT BREAKER INTERMITTENT (D-3). REPLACED CIRC
- [SDR ABXA010802](https://openairdocs.org/sdr/ABXA010802.md): Longeron · cracked · Mar 1, 2002 · N825AX · Doug DC863 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO, STATION 300 - 320, LONGERON 35 LEFT, ATTACH ANGLE CRACKED. REPAIRED AREA AND INSTALLED NEW SECTION OF LONGERON, NEW -Z- FITTINGS, SPLICES AND NEW WEB IAW DC-8 SRM 51-1-20D, 53-2-0, 51-1-8, 51-1-24 AND REA D853-43046MR.
- [SDR ABXA010806](https://openairdocs.org/sdr/ABXA010806.md): Fitting · damaged · Feb 25, 2002 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE FITTING (P/N 9755584-508) WAS DAMAGED. R&R IAW REA D853-43051-MR AND FAA FORM 8110-3.
- [SDR ABXA010654](https://openairdocs.org/sdr/ABXA010654.md): Light · inoperative · Dec 27, 2001 · N825AX · Doug DC863 · Smoke Detection
  > ON CLIMBOUT, UPPER CARGO SMOKE LIGHT CAME ON. NO SMOKE OR UNUSUAL SMELLS NOTED. NR 3 SMOKE DETECTOR APPEARED TO GIVE FALSE INDICATION. RELAMPED THE NR 3 UPPER CARGO SMOKE DETECTOR. OPS CHECKED GOOD IAW DC-8 MM 26-10-00.
- [SDR ABXA010450](https://openairdocs.org/sdr/ABXA010450.md): Control Box · defective · Aug 20, 2001 · N825AX · Doug DC863 · Landing Gear Position and Warning
  > RED GEAR UNSAFE LIGHT ILLUMINATED. LANDING GEAR AND DOOR LATCHING SELECTOR INDICATED RIGHT MAIN DOOR UNLATCHED. FOLLOWED ABNORMAL PROCEDURE AND ALL INDICATIONS RETURNED TO NORMAL. REPLACED THE GEAR PROXIMITY CONTROL BOX IAW DC-8 MM 32-10-00. OPS CHECKED GO
- [SDR ABXA010420](https://openairdocs.org/sdr/ABXA010420.md): Proximity Switch · malfunctioned · Aug 1, 2001 · N825AX · Doug DC863 · Landing Gear Position and Warning
  > AFTER GEAR RETRACTION RECEIVED RED GEAR UNSAFE LIGHT ILLUMINATION WITH UNSAFE LIGHT ILLUMINATED WITH GEAR UP. RAN ABNORMAL PROCEDURES AND RECEIVED RIGHT MAIN LANDING GEAR DOOR NOT LATCHED LIGHT MOMENTARILY THEN RIGHT MAIN LANDING GEAR DOOR LIGHT WENT OUT ACCO
- [SDR ABXA010410](https://openairdocs.org/sdr/ABXA010410.md): Uplock · out of adj · Jul 25, 2001 · N825AX · Doug DC863 · Landing Gear Retraction/Extension System
  > RED GEAR UNSAFE LIGHT CAME ON AT CRUISE AND THE RIGHT GEAR DOOR LANDING GEAR AND LIGHT WENT OUT. PERFORMED LANDING GEAR DOOR SWITCH TEST AND ADJ/TEST MAIN GEAR DOOR. CLOSED PROXIMITY SWITCH. BOTH CHECKED GOOD. ADJUSTED DOOR UPLATCH TURNBUCKLES IAW DC-8 MM
- [SDR ABXA010065](https://openairdocs.org/sdr/ABXA010065.md): Valve · defective · Feb 27, 2001 · N825AX · Doug DC863 · Master Cylinder/Brake Valve
  > THE LEFT MAIN LANDING GEAR WHEEL BRAKES WOULD NOT OPERATE. MAINTENANCE INSPECTED AND FOUND THE BRAKE HYDRAULIC POWER VALVE ASSY TO HAVE A BROKEN FORK. THE POWER VALVE WAS REPLACED IAW DC-8 MM 32-42-02.
- [SDR ABXA010004](https://openairdocs.org/sdr/ABXA010004.md): Window · stuck · Jan 9, 2001 · N825AX · Doug DC863 · Flight Compartment Windows
  > FIRST OFFICERS CLEARVIEW WINDOW DID NOT OPEN ALL THE WAY. MAINTENANCE INSPECTED AND REPLACED LOWER AFT HOOK SPRING AND ADJUSTED IAW DC-8 MM 56-10-03. PRESSURIZATION AND WINDOW OPERATION CHECKED GOOD.
- [SDR ABXA010002](https://openairdocs.org/sdr/ABXA010002.md): Window · stuck · Jan 9, 2001 · N825AX · Doug DC863 · Flight Compartment Windows
  > FIRST OFFICERS CLEARVIEW WINDOW WOULD NOT OPEN COMPLETELY. MAINTENANCE INSPECTED AND OPERATED THE FIRST OFFICERS CLEARVIEW WINDOW SEVERAL TIMES. THE WINDOW OPERATED NORMALLY IAW DC-8 MM 56-10.
- [SDR ABXA000360](https://openairdocs.org/sdr/ABXA000360.md): Window · out of adj · Aug 3, 2000 · N825AX · Doug DC863 · Flight Compartment Windows
  > FIRST OFFICER''S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED SERRATED HOOK STOP ON AFT OF FIRST OFFICER''S CLEARVIEW WINDOW. OPS CHECKED GOOD PER DC8 MM.
- [SDR ABXA000158](https://openairdocs.org/sdr/ABXA000158.md): Rack · malfunctioned · Mar 21, 2000 · N825AX · Doug DC863 · Emergency Lighting
  > EMERGENCY LIGHTS BLINKED ON/OFF EVERY 2.5 MINUTES. REPLACED EMERGENCY LIGHT RACK ASSEMBLY IAW DC8 MM, OPS CHECKED GOOD.
- [SDR ABXA000155](https://openairdocs.org/sdr/ABXA000155.md): Battery Pack · inoperative · Mar 20, 2000 · N825AX · Doug DC863 · Emergency Lighting
  > EMERGENCY BATTERY CHARGING CIRCUIT BREAKER WOULD NOT RESET. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC9 MM, OPS CHECKED GOOD.
- [SDR ABXA9900079](https://openairdocs.org/sdr/ABXA9900079.md): Spring · out of adjust · Feb 5, 1999 · N825AX · Doug DC863 · Landing Gear Door Retract Section
  > AFTER GEAR RETRACTION, RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR TWICE, UNSAFE LIGHT REMAINED. USED ABNORMAL PROCEDURES TO DETERMINE RIGHT GEAR DOOR UNSAFE AND SECURED DOOR TO NORMAL. ADJUSTED CABLE TENSION AND REPLACED OVERCENTER SPRING.
- [SDR ABXA9900126](https://openairdocs.org/sdr/ABXA9900126.md): Fitting · corroded · Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > BATHTUB FITTING CORRODED AT STATION 1220, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-20D AND ABX REA D853-24927-1MR.
- [SDR ABXA9900124](https://openairdocs.org/sdr/ABXA9900124.md): Fitting · corroded · Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > CORRODED BATHTUB FITTING AT LONGERON 28 LEFT, STATION 1260. REPLACED FITTING IAW DWG 3755842, ABX REA D853-24928 AND DC8 SRM 53-2-0.
- [SDR ABXA9900089](https://openairdocs.org/sdr/ABXA9900089.md): Fitting · corroded · Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > BATHTUB FITTING AT STATION 1260, LONGERON 30 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-21D, DWG 3755842 AND ABX REA D853-249271.
- [SDR ABXA9900088](https://openairdocs.org/sdr/ABXA9900088.md): Fitting · corroded · Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > EXFOLIATED BATHTUB FITTING AT LONGERON 29 LEFT, STATION 1220. REPLACED FITTING IAW ABX REA D853-24927 AND DC8 SRM 51-1-21D.
- [SDR ABXA9900087](https://openairdocs.org/sdr/ABXA9900087.md): Fitting · corroded · Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > CORRODED BATHTUB FITTING AT STATION 1200, LONGERON 29 LEFT. REPLACED FITTING IAW ABX REA D853-249279 AND DWG 93755842.
- [SDR ABXA9900086](https://openairdocs.org/sdr/ABXA9900086.md): Fitting · corroded · Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > EXFOLIATED BATHTUB FITTING AT STATION 1260, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 53-2-0 AND ABX REA D853-24921.
- [SDR ABXA9900085](https://openairdocs.org/sdr/ABXA9900085.md): Fitting · corroded · Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > EXFOLIATED BATHTUB FITTING AT STATION 1240, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 53-2-0 AND ABX REA D853-24927MR.
- [SDR ABXA9900083](https://openairdocs.org/sdr/ABXA9900083.md): Fitting · corroded · Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > CORRODED BATHTUB FITTING AT LONGERON 28 LEFT, STATION 1260. REPLACED FITTING IAW DWG 3755842, ABX REA D85324928MR AND DC8 SRM 53-2-0.
- [SDR ABXA9900082](https://openairdocs.org/sdr/ABXA9900082.md): Fitting · corroded · Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > BATH TUB FITTING CORRODED AT STATION 1220, LONGERON 31 LEFT. REPLACED FITTING IAW DWG 3755844, ABX REA D853-219271MR AND DC8 SRM 51-1-20D.
- [SDR ABXA9900125](https://openairdocs.org/sdr/ABXA9900125.md): Fitting · cracked · Jan 26, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > LEFT CUSP LOWER ATTACH FITTING CRACKED AT STATION 1080. REPAIRED IAW DC8 SRM 51-1-20D.
- [SDR ABXA9900084](https://openairdocs.org/sdr/ABXA9900084.md): Fitting · cracked · Jan 26, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > LEFT CUSP LOWER FITTING CRACKED AT STATION 1080. REPAIRED IAW DC8 SRM 51-1-20D.
- [SDR ABXA9900128](https://openairdocs.org/sdr/ABXA9900128.md): Bulkhead · cracked · Jan 23, 1999 · N825AX · Doug DC863 · Fuselage Main, Bulkhead
  > CRACKED INTERCOSTAL ON AFT BULKHEAD, STATION 1540 RIGHT. REPAIRED IAW DC8 SRM AND DWG 5646608.
- [SDR ABXA9900118](https://openairdocs.org/sdr/ABXA9900118.md): Gusset · corroded · Jan 23, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > GUSSET PLATE HAD EXFOLIATED CORROSION AT STATION 1240 LONGERON 24 LEFT. REPLACED GUSSETT IAW DWG 9755849 AND DC8 SRM 51-01-20D AND ABX RE AND 853-24930.
- [SDR ABXA9900117](https://openairdocs.org/sdr/ABXA9900117.md): Gusset · corroded · Jan 23, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous Structure
  > GUSSET HAD EXFOLIATED CORROSION AT STATION 1220 LONGERON 24 LEFT. REPLACED GUSSET IAW DC8 SRM 51-01-20D AND ABX REA D853-24930.
- [SDR ABXA9900116](https://openairdocs.org/sdr/ABXA9900116.md): Channel · cracked · Jan 23, 1999 · N825AX · Doug DC863 · Wing Miscellaneous Structure
  > LEFT MAIN LANDING GEAR SUPPORT STRUCTURE CRACKED AT AFT SIDE OF LANDING GEAR CUT-OUT. REPLACED CHANNEL IAW DWG 5611020 AND DC8 SRM 51-01-21.

Next page: https://openairdocs.org/deregistered/N825AX-2007-04-25/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N825AX' AND deregistration_id = 'N825AX-2007-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N825AX-2007-04-25/reports

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